MU-2 Magazine July 2015

JULY 2015 7th Edition

M a g a z i n e

What’s inside: º Maintenance: Hot Weather Engine Care º A Phantom Jet and a MU-2 / Wings & Rotors Air Museum º Reflections on Pilot Training º Sorrell’s Sideslips / New Feathers for an Old Bird º Technical: Recognizing Engine Failures

Photo: Howard Fields

MU-2 Owner/Operator

www.MU-2aircraft.com

Magazine

Published by Turbine Aircraft Services, Addison, Texas.

Editing and production by Mike Taylor, Connect Communications.

For subscription and advertising information: clcannon@turbineair.com or 972-248-3108. © 2015 Turbine Aircraft Services. All rights reserved. Reproduction in whole or in part of any text, photograph or illustration without written permission from the publisher is strictly prohibited.

Be On Your “A” Game At All Times We have just experienced one of the wettest Spring and Summer seasons that I can remember, throughout all of Central Texas. The lakes are overflowing in most places, and when coupled with the road construction going on throughout the region, this has severely hampered all modes of transportation. Just getting to the airport can be a challenge, so I’ll use this opportunity to remind you that we deal with frustrations like these every day no matter where we live and work.

fronts and thunderstorms, so you must be on your “A” game at all times.

SimCom. Ron tells it like it is.

This month for your enjoyment we provide you with a spotlight on owner/operator Rich Wall, who in addition to operating an MU-2, is deeply involved as the founder of the Wings & Rotors Air Museum in Murietta, California. Ralph Sorrells in his Sorrells’ Sideslips will bring you up to date on many MHIA projects that are in the works.

I think that you will once again enjoy a great variety of information and some fun stuff. Please let us know how you like the magazine, and let us know what we can do to make it better.

If you happen to be heading to the airport to command your MU-2 into the brighter skies, remember to leave all of those things that might have some effect on your performance on the ramp or in your car before strapping in behind the control wheel. We are, after all, human and tend to carry this baggage with us, sometimes to a not-so-perfect outcome. This is the weather season to contend with in terms of

Helmuth Eggeling’s Engines Part III, entitled Summer Engine Operations, brings us full circle through the seasons with which we deal while operating our MU-2. Rick Wheldon enlightens us with some great, and very timely, information on recognizing engine failures.

Pat Cannon

Finally, Ron Renz, who has recently joined the MHIA family, writes of his experiences during his Initial MU-2 training at

The Mitsubishi MU-2, one of Japan’s most successful aircraft, is a high-wing, twin-engine turboprop with a pressurized cabin. Work on the MU-2 began in 1956.

Designed as a light twin turboprop transport suitable for a variety of civil and military roles, the MU-2 first flew on September 14, 1963. More than 700 MU-2 aircraft were built before the aircraft went out of production in 1986.

Presently, nearly 300 MU-2 aircraft remain in operation with the majority of the fleet registered in the U.S.

www.mu-2aircraft.com

Pat Cannon is President of Turbine Aircraft Services. He is an FAA Designated Pilot Examiner, former MU-2 Demo Pilot, and Safety Expert.

Turbine Aircraft Services (TAS) is under contract to Mitsubishi Heavy Industries America, Inc. (MHIA) to assist with the support of the MU-2. TAS distributes MHIA issued publications and serves as liaison between MHIA and MHIA’s contracted Service Centers, Vendors and Training Agencies.

MU-2 Magazine, July 2015. Cover photo by Jan Glenn, taken during PROP photo shoot.

Notice: Although this publication will provide you with useful information regarding the operation of your airplane, it is not and cannot be a substitute for your compliance with all applicable requirements from the appropriate airworthiness authorities.

Turbine Aircraft Services • 4550 Jimmy Doolittle Dr. • Addison, Texas 75001 Tel 972-248-3108 • Fax 972-248-3321 • www.turbineair.com

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MU-2 Magazine - JULY 2015

Hot Weather Engine Care

By Helmuth Eggeling

N

Operations Spotlight

Helmuth Eggeling is a lead test pilot and pilot advisor for Honeywell Aerospace at Phoenix Sky Harbor International Airport. With the company for over 24 years, Eggeling conducts lectures and writes about engine operations for Honeywell turbine engine equipped aircraft. Born in Germany, he is a naturalized United States citizen and has logged more than 12,000 flight hours, including military time.

ow that summer is upon us and Indicated Outside Air Temperatures (IOAT) approach the +35° C (+95° F) range, a number of operational factors as they relate to TPE331 engine operations should be considered: NOTE: The information below is provided to aid you in the proper and efficient operation of your TPE331 engines as it relates to Hot/ Summer operations. However, as always, procedures outlined in the applicable FAA Approved Airplane Flight Manual (AFM) take precedence over those tips outlined in this article.

First, during summer, residual turbine temperatures remain at higher values for longer periods of time after engine shutdown.

Because post-shutdown turbine temperatures have shown to have a significant impact on the rate of fuel nozzle plugging, often referred to as coking, or baking-on a varnish-type of coating, inside the fuel nozzle passages, the use of specific procedures to control these temperatures becomes very important.

In fact, the relationship between peak temperature (heat soakback after engine shutdown) and coking rates is exponential. This implies that even a small reduction in peak temperature reduces the rate of coking substantially.

Two simple and common techniques involve the three-minute cool-down at low RPM before engine shutdown and the rotation of the engines by hand within approximately five minutes after engine shutdown. By adhering to both suggestions, the high point of the peak soak-back temperature can be reduced.

The practice of hand rotation is also commonly used to reduce the residual turbine temperature for subsequent starts on quick turnarounds. How many propeller blades the engine should be turned through, and how vigorously it is turned, is up to the operator. However, in general, three to four propeller revolutions (always in the designed direction of engine rotation) rotated “briskly”, is adequate.

In case a high residual temperature engine start is unavoidable, Honeywell suggests to first motor the engine (delaying fuel and ignition) until the turbine temperature is less than 200°C EGT or 300°C ITT (as applicable) or until 15 % RPM, whichever occurs first.

Second, during ground operations in high IOAT conditions, engine oil temperature may creep into the “high green” range.

Ambient factors such as wind direction and velocity contribute to the overall effect. Especially when the aircraft is static, such as during prolonged departure delays, the oil temperature may

increase slightly above normal. The radiator-type oil cooler is designed to regulate oil temperature. If that is insufficient, slightly advancing the power levers facilitates oil cooling in two additional ways: 1. The advanced power lever angle commands an increase in engine RPM, which enhances cooler efficiency.

2. In Beta-Mode of operation, the advanced power lever angle increases the propeller blade angle, thereby moving a greater volume of air across the engine nacelle and through the oil cooler radiator – that contributes to further oil cooling.

NOTE: Hot oil slightly lowers the effective governing speed while cold oil increases it. As a rule of thumb, an oil temperature 20° C higher than normal equates to approximately one-half percent RPM loss on some TPE331-powered aircraft.

The slightly increased engine RPM and the propeller-induced airflow offer several additional advantages. If the aircraft utilizes cooling turbine air conditioning, the elevated RPM increases the volume of bleed air available to the cooling turbine. This enhances environmental system performance and keeps the cabin and flight deck cooler. Also, the increased airflow across the engine nacelle reduces exhaust gas re-ingestion by the engine, which can cause incorrect inlet temperature sensing and tends to introduce a strong exhaust odor into the cabin air supply. In most instances the increase in RPM is barely noticeable to passengers.

Please bear in mind, when using increased RPM for ground cooling, professional airmanship would suggest consideration of the possible effect of increased propeller wake on other aircraft, personnel, or structures.

In conclusion, be cognizant of how high ambient temperatures affect engine operations and reliability. A few techniques can assist in efficient and more trouble-free engine operations.

However, this brief article deals only with a few high-temperature related engine issues. Therefore, the MU-2B airplane operator is advised to review all implications, AFM/POM procedures and other training manual suggestions associated with hot weather operations.

Please remember, the above tips are intended to be supplemental to the published operating procedures. For a complete study on aircraft operations in hot weather conditions, please refer to the FAA/CAA approved procedures and recommendations published in the Mitsubishi MU-2B AFM and POM for the appropriate model. As always, pilots can make the difference in engine operating life and maintenance costs.

For additional questions on the above subject or any other TPE331 engine related issues, please don’t hesitate to contact the Pilot Advisor Group by calling us at (602) 231-2697, send us a FAX to (602) 231-2380, or email: Helmuth.Eggeling@Honeywell.com.

MU-2 Magazine - JULY 2015

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...Nothing Prepares You Like Simulator Training.

A Phantom Jet and an MU-2, Both Merit Restoration to Keep on Flying

Owner/Operator Spotlight

By Mike Taylor Mike Taylor is a former aircraft design engineer, 25-year aviation industry veteran, private pilot and current marketing consultant.

T

he act of rebuilding something commands a leap of faith, strong determination, and a persistent belief that this something has merit. If not for such passion, entrusted to a select few individuals, the masterworks of our predecessors hasten to be forgotten. Significant pieces of history are lost.

Take for example the numerous historic aircraft that fill our museums and hangars. While a great many reside in welltrafficked places like the Smithsonian, countless artifacts remain hidden from public view. Oftentimes, though, uncommon collections exist in little known places, like your community airport.

Aircraft and collections spring from the obscure, and as such each historical piece has a unique story to tell. The vastness of historical artifacts struggle to be counted even in books. Importantly, those that do represent our current knowledge. Therefore, we must fully appreciate those individuals who devote themselves to history’s telling.

Well aware of this dilemma, one enthusiastic individual has taken upon himself the telling of a history to which he is innately connected. Rich Wall is in equal parts a builder, pilot and visionary. He’s also an MU-2 owner/operator and he inscribed to us at MU-2 Magazine, “Hey, if you are looking for other things to write about, check out my deal, wingsandrotors.org.”

Flying Has Its Steps As for many, Rich’s interest in flying began as a child. Later, as an adult, his passion was fed constantly. “I used to fly back and forth to work for several years in a Comanche 400 which I have logged about 3,000 hours in,” he said.

The Comanche 400 is a structurally strengthened (primarily in the tail) Piper PA-24 single-engine 4-seat aircraft with an aerodynamically balanced rudder. The PA-24-400 is powered by a, coincidentally, 400-horsepower 8-cylinder Lycoming IO-720 engine developed specifically for the Comanche. Produced from 1964 to 1966, only 148 were built. Due to high fuel burn (16 to 23 GPH), the aircraft was disparaged as expensive to operate. Top speed was 194 knots.

As his travel needs grew, including the need for more room for family, Rich was drawn to the MU-2. He was attracted by its short-field capability, and its greater power and speed. While investigating the possibility of acquisition, Rich heard the MU-2 had a reputation for being well-built and fun to fly.

Moving up in aircraft size and performance involves a series of steps. Rich explained, “Before buying my first MU-2, a broker took me for a demo ride in a King Air. I found out the Comanche was faster!”

Determination apparently being one of Thus, I was introduced Rich’s character traits, to Rich and set about he pushed forward familiarizing myself on the path to MU-2 with his exploits and ownership. “When museum. I quickly I went to look at the learned his is a Mitsubishi, I was told collection dedicated it is too hard to fly and uniquely to preserving that I’d need twinand flying Vietnamengine experience first.

Rich Wall sits in the Phantom F-4 he’s restoring for Wings & Rotors Air Museum. era fixed and rotary Well, I didn’t believe wing aircraft. Rich them.” He relished, Wall is also the CEO of two companies, Welded Fixtures and Rack “The MU-2 is the only twin I have flown. Having taken lessons in Displays. But it’s obvious that his current passions are consigned it after the purchase, 1,000 hours later I am still here.” to the museum he founded.

Rich juggles two jobs, his two companies, effectively one, and Rich was a teenager during the Vietnam War, thus explaining the museum. While the museum is something he’s passionate his inspiration for starting the museum. He articulated, “I got about, the work demands some creativity and challenges. Both lucky on draft lottery day and was number 300+. So I didn’t have companies are manufacturers of retail display fixtures. Welded to worry about getting drafted. Several friends did.” As Rich Fixtures is a custom shop that designs and builds large quantities described it, “The press made it into a bad situation. The soldiers of custom made-to-order displays, parts and printed products. were treated horribly.”

The other, Rack Displays, is Web-based where stock items are

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generally shipped to individuals.

Rich admits, “With the way the world is, most of the display business has gone to China. However, thanks to high shipping costs and longshoreman strikes, a lot of business has returned to the U.S.” He offered an example, “I have had to bail out customers on several occasions with time sensitive products that were stuck on a ship… good for me!”

A Passion For Flying Erupts In 1992, Rich seized an opportunity to travel to Russia and fly in an Su-27. “It was awesome to fly,” he remarked. “After that, I wanted a jet.” Thus initiated the impulse for Rich’s purchase of a Phantom F-4.

The Sukhoi Su-27 is a twin-engine supermaneuverable fighter aircraft conceived as a direct competitor to large, fourth-generation fighters such as the F-14. It was introduced in 1985 and used predominantly in Russia and China. Still in production, over 800 Su-27 aircraft have been built.

“The F-4 was in a guy’s backyard in the hills behind San Diego,” Rich said, “along with a B-24 he was restoring for a museum.” With an opportunity to buy the F-4, and it being from the Vietnam era, Rich envisioned a way to honor those of his generation. “I made a deal to get the F-4 and started restoring it in 2003. The museum’s F-4 stands today as a symbol of respect for those who served in the war,” stated Rich, reflecting on those less fortunate than he.

Rich Wall with the MU-2 he “salvaged” out of Africa and currently operates.

Rebuilding Is Second Nature Rich is by nature a compassionate and determined individual. He’s also intrinsically a builder. While his business centers on fabrication, thus making value out of what’s raw, with his museum Rich is a re-builder. He takes things discarded and gives them new purpose. “I didn’t want a graveyard for old aircraft. We work hard on the goal of keeping everything flying.

We are getting there with the F-4,” he confided.

“The aircraft in our museum exist for the enjoyment of our patrons, and their preservation should be seen as a benefit to anyone interested in their telling of the histories they carry,” he continued.

To Rich, the inspiration for maintaining aircraft is much the same as the inspiration

for building retail displays. With each completed project, he is enabling a story to be told. In the display business, a message is conveyed as the end result of its fabrication.

For The Love Of Flying Rich Wall founded Wings & Rotors Air Museum in 2005. However, his love of flying spans over 40 years. And the museum’s history reflects back on the era when Rich first started flying.

Wings & Rotors Air Museum is a nonprofit organization dedicated to restoring and showcasing Vietnam-era aircraft. The many people involved day-to-day with the museum’s activities take great pride in their work, striving for exact historical accuracy. Through extensive research and study, Rich and his staff learn about the aircraft with the goal of honoring the soldiers who used them.

The aircraft, their stories, and the museum stand, “In memory, from 1959 to 1975, of 58,479 brothers and sisters who never returned from the Vietnam War.” So states a marker in honor of the era.

Phantom BuNo 145310

Wings & Rotors Air Museum tells of the Vietnam War in honor of those who never returned.

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The museum’s centerpiece, a Phantom F4H-1 (Bureau No. 145310) was delivered to the Navy in August 1959 and was the 11th pre-production Phantom to be built.

It was used in different tests including weapons trials, carrier work, and some “Sageburner,” or speed record, trials.

MU-2 Magazine - JULY 2015

One of the Phantom prototype’s more memorable performances was demonstrating its bombing capability.

On April 22, 1961, it carried twenty-two 500-pound Mk 83 live bombs and dropped them at Fort Bragg, North Carolina.

Observing that day was President John F. Kennedy.

It was this demonstration that later sold the Phantom to the U.S. Air Force, filling its need for a hefty fighter-bomber. This 4.9-ton load, however, allowed for no external fuel and limited its combat radius. Later though, a mix of fuel plus bombs resulted in the F-4 being capable of delivering 8–10 bombs on target at a reasonable distance from the carrier.

During one of the weapons tests in 1961, BuNo 145310 (the museum’s F-4) launched a sidewinder missile and burned the paint clean off the bottom of the wing, landing gear door, and pylon. Also, in 1961, 145310 suffered an engine failure in flight, but the aircraft landed safely.

In 1964, the Navy was finished with its F-4 test aircraft, and 145310 saw its last flight in September of that year. It retired with less than 1,000 flight hours, and it would then spend the next 35 years in different storage locations throughout the U.S. BuNo 145310 had been declared military surplus, processed through the Defense Reutilization and Marketing Office, stricken from the inventory and basically was reduced in stature to scrap. It sat as a gate guard at one point, spent time in an East Coast museum storage yard, and eventually migrated west to Southern California.

One lucky day in 2000, a former Phantom Crew Chief and a couple of friends with financial backing, found BuNo 145310 in acceptable condition, and for an undisclosed amount purchased the aging Phantom. And so the journey began for this tired warrior and a new adventure.

The Disappearing Phantom QF-4 Rich is understandably proud of his museum centerpiece, the Phantom F-4. As a history buff with an affliction for unique aircraft, his passion extends to following the movements of the aircraft with which he’s been acquainted. Rich pointed out, “I

MU-2 Magazine - JULY 2015

just heard that the U.S. Air Force flew the last F-4, a drone, so the U.S. has no more flying.” (See USAF QF-4 Target Drones.)

But in spite of the demise of the F-4 and its drone use in the U.S., Rich informed me that these aircraft indeed still play a military role around the world. He noted, “The Iranians are still flying them, bombing ISIS locations in Iraq.” It is also reported that the Hellenic (Greek) AF operates 34 upgraded F-4E-PI2000 and 12 RF-4E aircraft as of September 2013.

Turkish F-4s remained in use as of 2015, until recent accidents led the TAF to withdraw its RF-4Es from active service.

Repeat Affair with an MU-2 and an Inclination Toward Restoration Rich owned his first MU-2 some 20 years ago and loved it. However, that aircraft was sold to start his Welded Fixtures business.

“When a deal came along ten years ago,” lauded Rich, he purchased an MU-2 for the second time. “I got the plane out of Africa and made a rebuild project out of it.”

Rich’s current MU-2, N770RW, is not the same aircraft that he had previously owned. He explained, “The one I have now was kind of left for dead, timed out in Africa where it served as a fly-around mobile hospital. It has amazing logbooks of daily half- to 3-hour flights all over Africa taking doctors here and there. The plane had all kinds of wiring in it, even out through the wing to power some kind of medical devices.

“It was in pretty bad shape when I got it. I was thinking it just needed to have the hot sections done and we would be good,” he divulged, adding that “inexperience” got him taken to the cleaners by a couple of “turbine engine hoodlums.” While the -6s were worn out, including their propellers, they were good for some parts. So, he traded the original -6 engines for complete -10s off a parted-out Marquise.

Pleased with his -10s, complete with 4-bladed props and good times remaining, Rich set forth re-wiring the MU-2. “This took the most time, particularly hooking up the SRL system (see footnote).” He continued, “I installed all new avionics and (Continued on page 16)

Supersonic F-4 Phantom The McDonnell Douglas F-4 Phantom II is a tandem two-seat, twin-engine, all-weather, long-range supersonic jet interceptor aircraft / fighter-bomber originally developed for the U.S. Navy by McDonnell Aircraft. It entered service in 1960 with the Navy and later the Marine Corps and Air Force, eventually playing a major part in each.

The Phantom is considered a large fighter with a top speed of over Mach 2.2. It can carry, externally, more than 18,000 pounds of weapons on nine hardpoints.

It set 15 world records for in-flight performance, including an absolute speed record, and an absolute altitude record. During the Vietnam War, the F-4 was used extensively; it served as the principal air superiority fighter for both the Navy and Air Force, and later ground-attack and aerial reconnaissance roles. 5,195 F-4 Phantoms were built from 1958–1981.

Project Sageburner In 1961, the Navy commemorated 50 years of Naval Aviation, sponsoring a project known as Sageburner. The project was designed to set new speed records, at low altitudes, flying F-4A Phantoms.

The initial attempt ended in tragedy as Commander J. L. Felsman was killed when a pitch dampener failure led to pilot-induced oscillations. However, the second attempt succeeded on August 28, 1961, when Lt. Huntington Hardisty (pilot) and Lt. Earl De Esch (RIO) flew F4H-1F BuNo 145307 at an average speed of 902.760 mph over a 3 km lowaltitude course at the White Sands Missile Range in New Mexico. The maximum altitude reached during this flight was only 125 feet, fully living up to the name of the project—Sageburner. The F-4A (BuNo 145307) was later turned over to the National Air and Space Museum and is preserved in storage at the Paul Garber Restoration Facility at Suitland, Maryland.

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MU-2 Magazine - JULY 2015

Reflections of a New MU-2 Pilot

Training Spotlight

By Ron Renz Ron Renz is a member of the engineering support team for the MU-2. He holds degrees in both Aerospace and Mechanical Engineering. Ron also carries an ATP certificate and is an A&P with Inspection Authorization. He has served as both a flight test engineer and pilot, and has worked on many STC programs involving computerized flight test equipment and specialized techniques for simulator data gathering of flight test programs.

I

have been involved with the MU-2B airplane for many years, working with the MHIA team to develop and produce several of the product improvement STCs that many of you are familiar with. I recently became a formal member of the MHIA product support team, supporting the engineering, FAA liaison and product improvement efforts. Because of that I recently had the pleasure to attend Simcom for MU-2B initial and differences training. I am a firm believer in simulator training, mentoring and regular recurrent training, and that is what this article is about.

the subject and specific to the airplane you are learning. These help the instructor to explain the systems. There are lots of comprehensive discussions of the airplane systems. It was very apparent that the instructor knew the airplane. The discussions bounced around the systems and provided much relevant and important information. If you’ve ever been through one of these courses, you realize that there is a lot to learn, and the 20 hours allotted is not enough to go through it all and completely understand the airplane.

Let me start by giving you all a little of my background as a pilot.

I’ve been flying since my first solo in 1974. I have an ATP license, Multi-Engine Land with type ratings on the Hawker HS125-1A and 800, the Boeing 737200 and Lear Jet 35. I have total time of about 5600 hours; 2800 hours of MultiEngine time and about 500 hours of turbine time in both turboprops and jets.

I own two airplanes that I regularly fly; a Piper Seneca for transportation and an aerobatic Christen Eagle for fun, excitement and regular upset recovery training.

Much of my flying time has been experimental flight test, and I’ve flown over 100 different types of airplanes.

Transitioning to new and different airplanes is a regular part of my flying life.

Simulator Sessions

The Simcom Training Program As most of you know, the Simcom MU-2B initial SFAR 108 training consists of a combination of classroom, simulator and airplane sessions. The training was spread over eight days.

Classroom time is approximately 20 hours, simulator instruction sessions approximately 20 hours (about 1/3 of the simulator session consisted of briefings, and 2/3 flying the simulator), and then three days with the airplane.

Classroom Sessions Classroom sessions utilize on-screen computer driven slides, with instructor-led discussions. Simcom also provides a comprehensive training manual. The presentation materials are relevant to

MU-2 Magazine - JULY 2015

Simulator time consisted of five sessions; one each day and approximately 1½ hours each. Sessions were well conducted; they were organized, and presented a good training scenario. There are obvious limitations to the Simcom simulator, as it is not motion based and does not have any kind of a ground handling model programmed, and therefore is unable to simulate any realistic ground operations. Hence, on the ground it is more difficult to maintain runway heading using only the nose wheel steering. In flight, the simulator is a reasonable representation of the airplane. Overall it provides a good and valuable training benefit. There are some minor discrepancies between the airplane and the simulator; however for an initial training program they are not really significant. Because of the FAA-dictated SFAR training requirements, there was much time spent on the required profiles, as there should be, but that made it challenging to try to cover every system failure and emergency. Those will certainly be covered in much more detail during my recurrent training.

Airplane Sessions Airplane sessions consisted of six flights spread over three days, totaling about 10 hours and 19 takeoff/landings. I used Turbine Aircraft Services’ (TAS) Solitaire, N400PS, which many of you are familiar with. As expected, the training was well conducted and provided the expected training benefit. Training consisted of air (Continued on page 15)

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MU-2 Magazine - JULY 2015

Sorrells’ Sideslips By Ralph Sorrells–MHIA Deputy General Manager

NEW FEATHERS FOR AN OLD BIRD

Just because our beloved MU-­‐2 recently celebrated 50 years since the first flight that was conducted in Nagoya, Japan during the early certification days it doesn’t mean that the ole girl is becoming “seedy” with age. Mitsubishi Heavy Industries America, Inc. (MHIA) is continuing with various programs to give her a “face lift” and at the same time, enhance safety. Many of you are aware of some programs that we have in play, but probably not all. Here is a list and current status:

1) Angle of Attack (AOA): A device to alert pilots as they approach a critical angle of attack is on the “DO LIST” by not only MHIA, but also the FAA, NTSB, AOPA, NBAA, GAMA and other alphabet groups. Our AOA system will be geared to provide visual and aural cues for all MU-­‐2 flap positions. MHIA Engineering has met with the FAA, an approval plan has been formulated and flight tests were completed by the end of June 2015.

Hopefully, MHIA will be able to announce availability by the next NBAA convention in November of this year.

2) Sniffle Valve: MHIA’s new vendor, Helimac, located in San Francisco, is currently working with MHIA to complete a First Article Inspection. Positive completion of this inspection in early June could mean parts will be available this summer.

3) Control Wheel: New technology in the form of 3-­‐D printing is being considered as a method to fabricate new replacement control wheel components. This project is in progress and is expected to be completed around the 2nd quarter of 2016. At that time parts will be available.

4) Stretched Acrylic Cockpit Side Windows: Perkins Aircraft Windows of Fort Worth, Texas will be our vendor for these windows. Prototype parts have been completed and fit tested on the MU-­‐2 airframe. Once a First Article Inspection and Conformity Inspection have been completed (expected in July 2015) and final FAA approval of an amended STC, MHIA hopes to be able to announce spare parts availability at the upcoming NBAA convention in mid-­‐ November.

5) Flexible Ducts, Hoses and Tubes: Industrial Tube Corporation (ITC) of Perris, California will be MHIA’s supplier of flexible ducts, tubes and hoses that are replacements for the 10-­‐year hose and tube replacement items. Currently, DAR conformity and FAA approval are necessary as a prerequisite to beginning the manufacturing and supply process. MHIA is hoping to announce spares availability in the 3rd quarter of this year.

So, while our ole MU-­‐2 birds might not be changed into “spring chickens,” where possible, MHIA wants to prevent ruffled feathers and keep your MU-­‐2 flying economically, safely and always as an enjoyable experience.

Keep ‘em Flying Safely

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We welcome all MU-2 owners and operators to join us in Aiken, South Carolina this October for a good time and Southern hospitality as we celebrate the aircraft we have all come to admire and respect.

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MU-2 Magazine - JULY 2015

Recognizing Engine Failures

By Rick Wheldon

Technology Review

Rick Wheldon is Vice President of Turbine Aircraft Services. He is a former Naval Aviator, Aeronautical Engineer, and MU-2 Demo Pilot.

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ecently, on the MU-2 blog, a Canadian Metro III accident report on a 2013 fatal accident at Red Lake, Ontario, Canada generated a spirited discussion. Because the Metro III uses the same engines as the MU-2, and because the Metro crew did not recover from an engine failure on approach, it seemed that this would be a good opportunity to investigate the crew’s actions and, perhaps, investigate how we can achieve a better outcome should this failure happen to any of us.

Bearskin Airlines Flight 311 suffered a significant loss of power to the left engine while on approach at about 500 feet AGL. The power loss was attributed to a crack in a fuel nozzle, causing streaking fuel, stator vane burn through, and a resultant first stage turbine wheel failure.

Without the first stage wheel producing power, the engine continued to run with the second and third stage turbine wheels still producing very limited power. The residual power being produced was not so low as to trip the NTS. It was a cold day, and the airport elevation of 1265 feet ensured that high power was available on the remaining engine.

Within three seconds of the engine failure, the pilot flying added full power to the right engine and raised the landing gear. With the consequent yaw, the power loss on the left engine would have been unmistakable. The airspeed at this point had only decayed 3 knots from the approach speed at the time of failure, and the airplane stayed relatively wings level (within 10 degrees bank) for 21 seconds after full power was set.

Let’s discuss engine failure recognition. In this accident, the crew almost immediately noted the failure and responded appropriately. They saw the power loss, immediately added full power on the remaining engine, and raised the gear. How was it that they recognized the engine failure? Even at low power on a normal approach, the torque on the left engine dropped from 22% to -1%. The aircraft would certainly have had to yaw with a

MU-2 Magazine - JULY 2015

sudden 23% power differential, and the yaw would have become even more apparent once power was added on the right engine.

The RPM on the failed engine dropped from 98.5% to 96%. These are 3 strong indicators of an engine failure. By their actions, there can be no doubt that the crew immediately knew there was an engine failure. Yet they failed to stop and feather the engine. Why? A very significant finding by the investigators was that many pilots interviewed believed that NTS protection would eliminate drag. NTS appears to have been working on this airplane, and the pilots may have relied on it for drag elimination. Unfortunately, their failure to stop and feather the engine (same as CONDITION LEVER…Emergency Stop) meant that a small but significant amount of drag that could have been eliminated was not. From the report: “The NTS system does provide partial anti-drag protection if negative torque is sensed, but not to the extent that is provided by a fully feathered propeller.”

In other words, NTS eliminates most of the propeller drag, but the propeller must be feathered to eliminate the rest. Because singleengine performance margins are small in most airplanes of this category, with low climb rates to be expected when operating single-engine, it becomes imperative that the engine is stopped and feathered to achieve maximum performance.

We might propose certain guidelines that can be used to determine a crew’s response to engine malfunctions. There are a number of failure modes on this engine, and for every one of them there will be multiple indications of the failure. These indications may be uncommanded power loss (torque drop), sudden yaw and roll, RPM change, a fire light, or uncommanded changes in fuel flow, EGT/ITT, oil temperature or pressure. You might note a surge, or an unusual sound or odor, or an auto(Continued on page 14)

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Recognizing Engine Failures (Continued from page 13) ignition light. If you note any two of these indications, you have an engine failure. If you only see one, you might have a faulty indication and elect to investigate further, but in any case, you can always advance the power levers of both engines and see if a yaw develops. Notice that we should not reduce power, as is commonly taught on piston twins. Certain gearbox failures for the TPE331 can increase drag if the power levers are retarded, so any single abnormal indication should be investigated once aircraft control is assured only by advancing the power levers. Let’s say this again. Never retard the power levers if you are investigating an engine problem.

When any engine failure is recognized, regardless of the failure mode, the only appropriate response should be to follow the Engine Shutdown procedure. With that in mind, let’s review some of the various failure modes.

First is a simple flameout. For whatever reason, the flame extinguishes or the airflow is disrupted and the engine loses power. Torque will immediately drop to slightly below zero, and the RPM and EGT/ITT will decrease. At high power, this will be accompanied by considerable yaw. The pilot will, of course, feel the yaw and also a slight but unmistakable cycling in yaw caused by the failed engine NTSing as the RPM drops. Even at flight idle, with just a slight yaw, the pilot still would see and hear uncommanded EGT/ITT and RPM drops, and feel the NTS surging. For high or low power, that’s more than two strong failure indicators, and an Engine Shutdown is warranted.

If there is a failure of the gearbox drive train, such as a prop shaft coupler or a ring gear failure, torque will drop to zero, the airplane will yaw, and the RPM will increase to 103-105% (overspeed governor setting.) Again, there are plenty of indicators to shut down the failed engine with the Condition Lever.

If a fuel control drive spline fails, the fuel control will sense zero RPM and add fuel in an attempt to return to “on speed.” Torque, EGT/ITT and fuel flow will all increase to very high numbers, well above engine limits, and the airplane will yaw. Again, shut down the failed engine with the Condition Lever. Note in this case the failed engine is producing excess power and the yaw is away from the failed engine.

This is contrary to the “dead foot, dead engine” mnemonic that many of us learned early on in our flying days. Therefore, the proficient TPE331 pilot will identify the failed engine using engine instruments and not by using the “dead foot” criteria.

Finally, let’s look at the Red Lake failure mode. The near total failure of the 1st turbine with the 2nd and 3rd turbines still producing power, and the fact that the functioning NTS did not actuate, says that the engine was producing slightly more torque than would be required to trip the NTS. This still would leave plenty of indications to shut down the engine. First, there was an uncommanded torque drop. Second, there was a slight yaw, which would have become greater when power was added after the failure. More subtle but still noticeable, the RPM dropped 2

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1/2 % at the time of failure. Not stated in the accident report, but most likely also true, is that the left EGT would probably have been abnormal. We’ve just listed several indications of a failure, any two of which should cause us to place the Condition Lever to Emergency Stop. As noted earlier, the crew did recognize this failure but for some unknown reason failed to stop and feather the engine.

Let’s go back to the moment of failure. Once an engine failure is recognized, Rule #1 is always FLY THE AIRPLANE! Add power, maintain airspeed, maintain control, carefully raise the nose to a go-around attitude, and raise the landing gear (and retract the landing lights) to reduce drag. Now, once the failed engine has been positively identified, use the Engine Shutdown procedure.

There are only two memory items, and the first item takes care of the remaining propeller drag – Condition Lever to Emergency Stop.

Closely following the reasoning in the preceding paragraph, and very significant in the accident report, is a new procedure that was added to Bearskin’s manual – Engine Failure on Approach. These are the memory steps for that new procedure: 1. POWER INCREASE TO 60% TORQUE OR HIGHER AS REQUIRED 2. LANDING GEAR UP 3. FLAPS 1/4 4. STOP AND FEATHER (failed engine) PULL 5. LANDING GEAR (landing assured) DOWN 6. FLAPS AS REQUIRED Essentially, steps 1-4 now require the crew to initiate a singleengine go-around, raise the gear to reduce drag, and SHUT DOWN THE ENGINE! Only after the go-around is initiated do steps 5 and 6 allow a subsequent reversion to an approach mindset, and then only after the pilot has determined that the landing is assured.

A pilot should normally be spring-loaded for a single-engine go-around/engine shutdown whenever an engine fails in the landing pattern. Approach preparation should include checking the single-engine climb charts to ensure that the airplane is capable of a single-engine climb at the current weight, altitude and temperature (otherwise landing straight ahead, under control becomes the only option.) The transition from a two-engine to a single-engine profile in the last 1000 feet of an approach places a high workload on the pilot, requires great finesse, considerable but precise power, trim and control changes, an engine shutdown, and allows for no preparation for the approach. In contrast, a simple go-around allows a pilot to climb out, get comfortable with the procedures, carefully review and complete the single-engine landing checklist, then plan and conduct a single-engine landing after much better preparation. The single-engine go-around should be part of your tool bag.

MU-2 Magazine - JULY 2015

Reflections of a New MU-2 Pilot (Continued from page 9) work (the usual steep turns, stalls and VMC demonstration, and other single engine operations. SFAR 108 maneuvers were used as the primary basis of defining and measuring performance during these maneuvers).

route,” take the time to get proper training from a qualified individual or entity who knows the airplane well. My preference is simulator-based training. You can do things in the sim that you would never try in the airplane. My other observations are:

Next we moved on to the runway and approach phase of the training. As expected, the usual ILS and non-precision approaches with both two-engine and single-engine operations were performed. The only real surprise for me was the frequency of trimming required to proficiently manage the airplane. The MU2B airplane requires more precise trimming to make it easy to fly.

This is quite different from the other airplanes that I have flown, and it is the only real difference between the MU-2B and the other airplanes I have flown. Once that is learned, the MU-2 is as manageable as any other high performance airplane.

1) The Sim is real and accurately represents the airplane;

Training Result My final training flight was the SFAR 108 final phase check. As a result of the training, this check was successful. I came out of this training confident that I could safely operate the MU-2B. Recommendation As with any high performance airplane, I believe that for a pilot new to the airplane, more experience in real world day-to-day operations is still needed, especially before flying off into difficult or challenging weather or in higher traffic environments. As with all concentrated training programs, regardless of where you go, or who your instructor is, training cannot fully accomplish exposure to the real flight planning and day-to-day choices that may be needed in order to operate the airplane at the highest level of safety and efficiency. There just isn’t the time.

2) You should try to spend more time in the sim than the minimum; 3) Dedicate your evenings before, during and after the training to serious study, and read the manuals. Get to know what’s in the book and where you can find it. There is a wealth of information in both the AFM and POM of the MU-2B; 4) Find a good mentor pilot. Fly with him or her for the first 25 to 50 hours on real trips, in real weather and in real congested terminal areas. Continue to fly with that mentor until you are confident that you know, understand and appreciate the airplane.

I have found that most airplanes take in the order of 50 to 100 hours before you truly understand their nuances and quirks; and, 5) Enjoy the airplane. MU-2B owners love their birds for very good reasons. Learn to get the most from the airplane and it will give back to you every effort you put in… IN SPADES.

Training environments, out of necessity, concentrate operations on less realistic scenarios that do not reflect the normal day-today operation of the airplane. Most insurance companies require, and most professional pilots realize, that mentoring flights with an experienced supervision pilot for this class airplane is invaluable and a necessity. I agree. My past experience has shown that somewhere in the order of 25 to 100 hours is needed (depending, of course, on the airplane type and the pilot’s experience). All the past high performance airplanes I have flown are no different, and that is what I do whenever I transition to a new airplane type.

I have personally experienced that the first several flights in a new airplane often present unexpected challenges which were not covered in the training. When this happens, it is good to have an experienced mentor beside you to help you learn and safely manage these challenges. The more experience one has with the airplane, the less critical these challenges become, and soon you will be a safe and competent pilot in the new bird.

Closing Thoughts In case you haven’t figured it out, the message that I leave here for any potential new MU-2B pilot is as follows... Regardless of whether you go the simulator route or the “only in the airplane

MU-2 Magazine - JULY 2015

Ron Renz in the cockpit of his Christen Eagle aerobatic biplane.

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A Phantom Jet and an MU-2 (Continued from page 7)

USAF QF-4 Target Drones

interior. Today, I have about 1,000 hours of MU-2 time. It was the first twin I ever flew.”

Designated QF-4 (the “Q” prefix signifies a drone conversion), the Phantom II served as a drone at the end of its days.

Beginning in 1995, over 230 Phantoms were “droned.” At a cost around $800,000 per aircraft, the modification equipped the retired jets with a digital control system allowing remote operation of the aircraft’s steering, throttles, flaps, landing gear, brakes, braking parachute, and tailhook. Wingtips and tail were painted orange to distinguish the aircraft as a drone. The QF-4s were almost always flown with a pilot aboard, unless a weapons launch was to occur. Hands-off, the pilots sat ready to take over if ground control was lost or the aircraft departed.

However, pilots would fly the aircraft themselves on chase missions and to maintain proficiency. Drone controllers would have a flight instrument display on a monitor, but no direct visual contact with the aircraft, flying with a joystick, keyboard, throttles, and rudder pedals.

Most test and evaluation flights were steered by computer, at times allowing up to six QF-4 aircraft to be controlled in formation. Operators relied on GPS to maintain each aircraft in position relative to the flight track.

Though the MU-2 project had many hurdles, Rich noted it was not without humor. “While the aircraft sat in primer gray for several years, one of my guys painted a big red Japanese meatball on the side for fun.” He concluded, “The rumors at the airport had it that I was re-building it for the Japanese Air Force!”

An Inclination Toward Restoration and a Passion For Preservation The F-4 now at Wings & Rotors Air Museum is housed with three additional Vietnam-era aircraft, all whirlybirds. These include: 1) a piston-engined Sikorsky H-34 Choctaw, 2) a Bell UH-1B “Huey” assault model of the U.S. Army, and 3) a Bell OH-58A (model 206, akin to the civilian derivative Jet Ranger) “Kiowa” Light Observation model of the U.S. Army.

The Phantom F-4 has a great storied history and we are fortunate for folks like Rich who are dedicated to telling it. Rich summarized, “Both the MU-2 and the museum represent what I like to do, which is to rebuild things.

“The F-4 and the Huey were the same way.

I’ve enjoyed rebuilding them and making them fly, well almost flying, as with the Phantom. The Phantom’s jet engines are at the overhaul shop. I’m hoping to have them re-sealed and run on the test stand later this year. Engines are the last hurdle.

Everything else is in place and we are hoping to have it flying by the end of the year.”

The museum occupies two hangars at French Valley Airport, in Murrieta, California (midway between Los Angeles and San Diego off I-15). Hours are Monday–Friday, between 9 am and 4 pm.

All visitors are welcome.

All aircraft are kept in operational condition and are frequently used in airshows. For more information, go to wingsandrotors.org or visit Wings & Rotors Air Museum at: 37350 Sky Canyon Dr. Hangar 7, Murrieta, California 92563 Thanks to Rich Wall and the Wings & Rotors crew for sharing their passion for flying and its history. www.weldedfixtures.com www.rackdisplays.com

L-R: Jen Franklin, Museum Administrator; Richard Wall and wife Vicki; and Pat Rogers, Museum Director and Crew Chief pose with the museum’s Sikorsky H-34 Marine helicopter.

SRL, or Single Red Line, is a computerized engine temperature indicating and control system. The SRL system provides a single reference value for gauging engine performance, in this case, the EGT. It became standard issue on Solitaire and Marquise models.

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MU-2 Magazine - JULY 2015

MU-2 Magazine - JULY 2015

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